AIRFOIL ASSEMBLY

VARIABLE PITCH AIRFOIL

AIRFOILS FOR GAS TURBINE ENGINES

Interspacer

INJECTION BONDING OF COMPOSITE VANE INTO POCKET

Propulsor Fan

FLUID TURBINES

ROTOR BLADE DETACHMENT DEVICE AND ROTOR BLADE DETACHMENT METHOD

TEST BLADE FOR GAS TURBINE ENGINE AND METHOD OF MAKING

AIRCRAFT TURBOMACHINE HAVING VARIABLE-PITCH PROPELLER VANES

FAN BLADE OR VANE WITH CROSS-SHAPED OR STAR-SHAPED COMPOSITE ROOT

TURBINE ROTOR DOVETAIL STRUCTURE WITH SPLINES

PROPELLER BLADE OR VANE HAVING A HOLLOW COMPOSITE ROOT

COMPOSITE BLADE

SYSTEM FOR ATTACHING A TURBOMACHINE BLADE

VARIABLE PITCH AIRFOIL

TURBINE ROTOR BLADE

Matavian Propeller

TEST BLADE FOR GAS TURBINE ENGINE AND METHOD OF MAKING

ANNULUS FILLER FOR A GAS TURBINE ENGINE

Turbine rotor dovetail structure with splines

GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY

PROPULSION SYSTEM AND METHOD FOR OPERATION

FLUID TURBINES

ANNULUS FILLER FOR A GAS TURBINE ENGINE

ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

Test blade for gas turbine engine and method of making

TEST BLADE FOR GAS TURBINE ENGINE AND METHOD OF MAKING

METHOD FOR PREPARING A ROOT OF A TURBOMACHINE BLADE

Rotor and aircraft

SYSTÈME PROPULSIF AÉRONAUTIQUE

Composite airfoil assembly having a dovetail portion

Split piston ring seal for a rotating assembly and method of sealing

Deformable root spacer for a gas turbine engine rotor blade

Fan blade for a gas turbine engine

Blade provided with a root comprising an integrated pitch attachment and two integrated damper attachments, and a rotor provided with such a blade

Rotor assembly for a gas turbine engine

Method for repairing an end plate of a turbomachine rotor

PROPELLER, PROPELLER KIT, POWER ASSEMBLY, POWER KIT AND UNMANNED AERIAL VEHICLE

COMPOSITE THERMOPLASTIC ROTOR BLADE WITH INTEGRAL CUFF

Propulsor Fan

Guide vane wheel of a turbomachine

BLADE PLATFORM, BLADE RING, IMPELLER DISK AND GAS TURBINE ENGINE

ADVANCE RATIO FOR SINGLE UNDUCTED ROTOR ENGINE

Rotatable Blade Apparatus With Individually Adjustable Blades

Method for manufacturing a turbine engine vane

System for controlling the pitch of a propeller vane for an aircraft turbine engine

INSPECTION SYSTEMS AND METHODS WITH AIRFOIL SHEATHS

AIRCRAFT TURBINE ENGINE COMPRISING VARIABLE-PITCH PROPELLER VANES

Assembly comprising a vane and a vane pitch setting system

Aircraft turbine engine comprising variable pitch propeller blades

Structure for assembling turbine blade seals and gas turbine including the same

Turbine blade and method for machining same

Blade pivot with adjustable orientation and protected integrity for a turbomachine fan hub

Impeller for aircraft engine

Bladed disc

Composite blade for a turbine engine rotor

SYSTEM AND METHOD OF PHASED ARRAY ULTRASONIC INSPECTION OF TURBINE BLADES

Jig for assembling and extracting blade root spring, and method for assembling and extracting blade root spring

Solution for manufacturing a one-piece bladed disc

AIRFOIL ARRANGEMENT FOR A GAS TURBINE ENGINE UTILIZING A SHAPE MEMORY ALLOY

Turbine rotor wheel for an aircraft turbomachine

HYBRID SUPERALLOY ARTICLE AND METHOD OF MANUFACTURE THEREOF

Propeller, propeller kit, power assembly, power kit and unmanned aerial vehicle

Turbine engine blade with improved cooling

Precision blade pitch adjustment

INJECTION BONDING OF COMPOSITE VANE INTO POCKET

One piece casting fan hub

Method of manufacturing a fan assembly

Turbine blade platform cooling holes

Aircraft turbomachine rotor comprising a damping device

ROTATABLE BLADE APPARATUS WITH INDIVIDUALLY ADJUSTABLE BLADES

HYBRID VANES FOR GAS TURBINE ENGINES

Blade dovetail and retention apparatus

ROTOR BLADE FOR A GAS TURBINE ENGINE HAVING A METALLIC STRUCTURAL MEMBER AND A COMPOSITE FAIRING

Propeller blade assembly

Rotor and turbo machine including same

Blade dovetail and retention apparatus

Blade dovetail and retention apparatus

Ram air turbine blade platform cooling

One piece casting fan hub and method of manufacture a fan

Moving blade for a wheel of a turbine engine

Jig for vibration test of rotor blade

Hybridization of fibers of the fibrous reinforcement of a fan blade

Characteristic distribution for rotor blade of booster rotor

Turbomachine rotor assembly

Fastener arrangement for rotating group of turbomachine

Rotor disc with axial retention of the blades, assembly of a disc and a ring, and turbomachine

Layered fuselage shield

Sealing washer for a rotor, and rotor with such a washer

AXIAL IMPELLER

Extended root region and platform over-wrap for a blade of a gas turbine engine

Blade with wearable tip-rub-portions above squealer pocket

Gas turbine engine with clutch assembly

Gas turbine engine outlet guide vane assembly

Seal element for sealing a joint between a rotor blade and a rotor disk

Rotor assembly with multiple rotor disks

Turbomachine rotor blade with an airfoil having a variable elliptical trailing edge

GAS TURBINE ENGINE FAN

Work station for electrochemically machining a workpiece, in particular a rotationally symmetrical workpiece, comprising a plurality of recesses, and method for producing an end contour of a recess

System and method for control for unducted engine

Composite blade and method for producing composite blade

Mount for an airfoil

Ceramic matrix composite blade track with mounting system having axial reaction load distribution features

Main rotor blade and helicopter

PROPELLER ASSEMBLY, POWER ASSEMBLY, AND AIRCRAFT

Fan blade attachment root with improved strain response

Rotor for turbine engine and turbine engine comprising this rotor

Gas turbine engine with a double wall core casing

Steam Turbine Rotor and Steam Turbine

Propeller, propeller kit, power assembly, power kit and unmanned aerial vehicle

Moving blade of a turbo machine

Inner shroud assembly for stator vanes

Inserts for slotted integrally bladed rotor

Method of manufacturing a fan assembly

Turbomachine stage and method of making same

Method for producing blades from Ni-based alloys and blades produced therefrom

FIR TREE ROOT FOR A BLADED DISC

Method for Optimizing Multi-Stage Components of Large-Scale High-Speed Rotary Equipment Based on Monte Carlo Bias Evaluation

Compressor rotor stack assembly for gas turbine engine

Blade of a turbine engine having a chord law for a high flutter margin

Rotor blade arrangement

Blade comprising an improved cooling circuit

Airfoil having integral fins

Rotor, power assembly and air vehicle

Turbine rotor disk blade having a foot of curvilinear shape

Compressor impeller, compressor, and turbocharger

REDUCED STRESS IN COMPRESSOR DISC

Vane platform leading edge recessed pocket with cover

Composite blade and method of manufacturing composite blade

First stage turbine blade

Composite vane with metal reinforcement, and its method of manufacture

Fan blade attachment root with improved strain response

Integrated strut and IGV configuration

Method for clear position determination and identification of a turbine blade

Method for disassembling/assembling gas turbine, seal plate assembly, and gas turbine rotor

Turbine vane including a cooling-air intake portion including a helical element for swirling the cooling air

Method for disassembling/assembling gas turbine, gas turbine rotor, and gas turbine

Fan spacer for a gas turbine engine

Fan for a turbomachine

AEROFOIL JOINT RECESS

Mounting tool for grooved pieces

Blade and method for reloading an abradable coating

Annulus filler

Rotatable blade apparatus with individually adjustable blades

Turbomachine with alternatingly spaced turbine rotor blades

Turbomachine with alternatingly spaced turbine rotor blades

Turbomachine with alternatingly spaced turbine rotor blades

Turbomachine with alternatingly spaced turbine rotor blades

Contact interface for a composite component and methods of fabrication

Fan assembly and method

Turbine for a turbine engine

Hub for propeller having variable-pitch blades, with radial and axial dimensioning variation

Fan Assembly and Method

CMC blade with internal support

Compressor rotor stack assembly for gas turbine engine

Method for removing turbine blade, removal device for executing said method, and rotor set with said removal device

Method of manufacturing a fan blade

A RADIAL TURBINE IMPELLER AND A METHOD FOR MANUFACTURING THE SAME

Stator assembly with retention clip for gas turbine engine

Stator assembly with contoured retention clip for gas turbine engine

I beam blade platform

Gas turbine engine component incorporating a seal slot

Torque converter including inertia ring connected to a turbine by a extruded rivet weldless connection

Turbomachine blade and relative production method

Compressor blade locking mechanism in disk with tangential groove

Turbomachine stage and method of making same

High temperature compliant metallic elements for low contact stress ceramic support

Additively manufactured blade extension with internal features

Transfer of turbine blades to rotor wheel

METHOD FOR PRODUCING A TURBINE BLADE BY MEANS OF ELECTRON BEAM MELTING

Blade of a rotary flow machine with a radial strip seal

Linear friction welding apparatus

Turbine wheel with circumferentially-installed inter-blade heat shields

Turbine blade mounting structure

Apparatus and system for marine propeller blade dovetail stress reduction

Propeller assembly and method of assembling

Attachment system for a turbine airfoil usable in a gas turbine engine

System and method for HPT disk over speed prevention

Rim seal for gas turbine engine

Intermittent tab configuration for retaining ring retention

Blade or guide vane with raised areas

Composite rotatable assembly for an axial-flow compressor

Blade for a Wind Turbine

Method for determining vibratory contact stress at a blade attachment

Airfoil with cooling circuit

Airfoil machining

Method for manufacturing shaft body

Shield member and jet engine using the same

Turbine rotor assembly, turbine, and rotor blade

Fan blade removal feature for a gas turbine engine

Method of forming aluminum alloy airfoils

Torque converter turbine including added mass

In situ tip repair of an airfoil tip in a gas turbine engine via frictional welding

Mobile vane for a turbine engine, comprising a lug engaging in a locking notch of a rotor disk

Turbomachine stage

Method and system for separable blade platform retention clip

Aero engine rotor assembling method and device based on concentricity and verticality measurement

Fan for a turbomachine

Stacking of rotor blades on centroids

Damper seal installation features

Rotor assembly for use in a turbofan engine and method of assembling

Dual alloy bladed rotors suitable for usage in gas turbine engines and methods for the manufacture thereof

Turbine blade attachment mechanism

Fabrication of gas turbine engine components using multiple processing steps

Rotating blade

Method and system to repair outer periphery of a body

Additively manufactured bladed disk

Support device, turbine, and support method

Rotor blade with wheel space swirlers and method for forming a rotor blade with wheel space swirlers

Component construction, component for a gas turbine and method for manufacturing a component of gas turbine by metal injection moulding

Fan blade attachment root with improved strain response

Turbomachine blade

Gas turbine bucket shanks with seal pins

Rotor damper

Rotor damper

Fixture for electro-chemical machining electrode

Rotary assembly for an aviation turbine engine, the assembly comprising a separate fan blade platform mounted on a fan disk

Nonmetallic airfoil with a compliant attachment

Bladed disc

Rotor disc

Method of mounting a turbine wheel axial retention device

CMC blade with monolithic ceramic platform and dovetail

Optical measurement system for detecting turbine blade lockup

Laser measurement system for detecting turbine blade lockup

Rotatable blade apparatus with individually adjustable blades

Dismantling device for blades and corresponding dismantling method

Abrasive flow media fixture with end contour

Turbine disk assembly including seperable platforms for blade attachment

Turbine rotor nut and bolt arrangement with improved fatigue resistance under centrifugal load

Turbine engine comprising a device for braking the fan rotor

Slider for chocking a dovetail root of a blade of a gas turbine engine

Plate for metering flow

Diaphragm assembly bolted joint stress reduction

Panels of a fan of a gas turbine

Turbomachine blade assemblies

Lightweight blade for gas turbine engine

Fan hub design

Engine component having support with intermediate layer

COATING PROCESS AND COATED ARTICLE

Turbomachine blade arrangement with first and second guides with respective movable first and second elements to reduce vibrational response

TRANSIENT LIQUID PAHSE BONDED TURBINE ROTOR ASSEMBLY

Turbine engine hybrid rotor

Composite airfoil bonded to a metallic root

Gas turbine spindle bolt structure with reduced fretting fatigue

Rotor assembly for gas turbine

Rotor blade root spacer with grip element

Gas turbine engine nose cone attachment

Turbomachine rotor blade, turbomachine rotor disc, turbomachine rotor, and gas turbine engine with different root and slot contact face angles

TURBINE BUCKET ASSEMBLY AND TURBINE SYSTEM

T-shaped platform leading edge anti-rotation tabs

Blade anchored securely in radial translation, propeller, turbine engine and aircraft

High temperature compliant metallic elements for low contact stress ceramic support

Method for manufacturing a turbine engine blade root of a composite material and blade root obtained by such a method

Aerofoil blade

Spinner for electrically grounding fan blades

Root lightening holes with slot

Steam turbine with resonance chamber

Flow rate responsive turbine blades and related methods

Axially-split radial turbines

Turbine bucket and method for balancing a tip shroud of a turbine bucket

TURBINE ROTOR OF AN EXHAUST-GAS TURBOCHARGER

Contoured flowpath surface

Mechanical Interlock Feature for Multi-Material Airfoils

Blade with redundant anchoring in a hub, propeller, turboprop engine and aircraft

Methods and apparatus for sealing a gas turbine engine rotor assembly

Twisted blade root

Aerodynamic root adapters for wind turbine rotor blades

ROTOR HAVING A BASIC ROTOR BODY AND A PLURALITY OF ROTATING BLADES MOUNTED THEREON

Template for aligning surface features on a rotor blade

Adjustable blade root spring for turbine blade fixation in turbomachinery

Wind spinner

Axial rotor portion and turbine rotor blade for a gas turbine

TURBINE BLADE

Blade of a rotary flow machine with a radial strip seal

Method for repairing wear marks on a rotor supporting the fan of a bypass engine

Mechanical joining using additive manufacturing process

Fan assembly

Turbomachine rotor blade

Closure bucket for turbo-machine

Ni based forged alloy, and turbine disc, turbine spacer and gas turbine each using the same

SHROUD ARRANGEMENT FOR A FLUID FLOW MACHINE

Rotor blade assembly having a stiffening root insert

Turbine engine wheel, in particular for a low pressure turbine

Bi-cast turbine rotor disks and methods of forming same

Turbine engine blade

Integral fan blade wear pad and platform seal

Blank casting for producing a turbine engine rotor blade and process for manufacturing the rotor blade from this blank

Systems and method for a composite blade with fillet transition

Attachment feature of a gas turbine engine blade having a curved profile

System for specifying an installation position of rotor blades, securing element, rotor blade, turbomachine, and method

Turbomachine blade and relative production method

Turbomachine blade and relative production method

Drum rotor dovetail component and related drum rotor system

MODULAR BLADE OR VANE FOR A GAS TURBINE AND GAS TURBINE WITH SUCH A BLADE OR VANE

Ceiling fan blade

Aircraft rotor blade and relative forming method

Airfoil member and composite platform having contoured endwall

TURBOMACHINE AND METHOD OF HANDLING TURBOMACHINE COMPONENTS

Ni-Based Heat Resistant Alloy, Gas Turbine Component and Gas Turbine